# STC SA4444NM

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Craner Robert A, United States
- Description: Installation of McCauley B3D34C405/90DFA-13 propeller.
- Applied: August 20, 1980
- Status date: July 9, 1982
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A12SO](https://openairdocs.org/tcds/A12SO)
- Certificate PDF: https://openairdocs.org/files/sha256/a7/e7/a7e725cea621840bebc187f305e837a01ee40d40a94e760bfe08bf1c34766512
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/38521B165BAF5BD085256CC2000E3C80.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA4444NM

## ADs that name it (0)

None.

## Approved models (1)

- Commander Aircraft Corporation 114 ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SAA944NM This certificate issued to: Robert A. Craner Part 23 of the Federal Aviation Regulations: See T.C. Data Sheet A12SO for complete certification basis.

Original Product -Iype Prentificato Number: A1250 Make: Gulfstream American (Rockwell Int.l') Merted: 114 Despilen he dinin FA sealed All Aircraft Services R. Craner Installation of McCauley B3D340405/90DFA-13 Propeller Installation Instructions #1, dated July 2, 1982 or later FAA approved revision.

Robert A. Craner FAA approved Airplane Flight Manual Supplement dated JUL 9 1982 is required.

Limitations and Conditions: The approval of this change in type design applies to the basic aircraft of the specified model that is otherwise unmodified. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

Date of Application: AUgUSt 20, 1980 Date Reissued:

Date of Issuance: JUlY 9, 1982 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Lyle C. Davia (Signature ) TEMNISTRAIO Retingenies, Aircraft Modification section 47 FAA FORM 8110-2 (10-68)

## Every issue (1)

- July 9, 1982: Issued, Current. [certificate](https://openairdocs.org/files/sha256/a7/e7/a7e725cea621840bebc187f305e837a01ee40d40a94e760bfe08bf1c34766512)

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